Experimental and numerical analysis on tonal noise of single-stage axial compressor

被引:0
|
作者
Chen C. [1 ]
Wang Y. [2 ]
Shu W. [1 ]
Du L. [2 ]
Sun X. [1 ,2 ]
机构
[1] School of Energy and Power Engineering, Beihang University, Beijing
[2] Research Institute of Aero-Engine, Beihang University, Beijing
来源
关键词
compressor; noise prediction; rotor-stator interaction; tonal noise; unsteady pressure fluctuation;
D O I
10.13224/j.cnki.jasp.20220903
中图分类号
学科分类号
摘要
To investigate the correlation between the tonal noise generated by rotor/stator interaction and the incoming upwash velocity of the stator, the tonal noise of a single-stage, low-speed axial compressor test rig (TA36) in a throttling process was studied by a well-developed inhouse hybrid noise prediction method. In order to accurately capture the source of the tonal noise, i.e., unsteady pressure fluctuation on the surface of the stator blade,the effects of the simulation grid and time-step size on the prediction of the unsteady pressure fluctuation were discussed firstly. Then, the variations of upwash velocity and tonal noise in the throttling process were compared. The result showed that at the third blade passing frequency (BPF) of the design speed,the amplitude variation of the incoming upwash velocity on the 70%,80%,and 90% span of the stator was consistent with the sound pressure level predicted by the hybrid method, and kept good consistency with the experimental measurements. In addition, the sound radiation in the far field demonstrated significant directivity while the directivity did not change significantly with the mass flow rate. © 2023 BUAA Press. All rights reserved.
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页码:1239 / 1249
页数:10
相关论文
共 28 条
  • [1] PEAKE N,, PARRY A., Modern challenges facing turbomachinery aeroacoustics, Annual Review of Fluid Mechanics, 44, pp. 227-248, (2012)
  • [2] (1993)
  • [3] (2014)
  • [4] (1993)
  • [5] HEIDMANN M F., Interim prediction method for fan and compressor source noise, (1975)
  • [6] KONTOS K B, JANARDAN B A, GLIEBE P R., Improved NASA-ANOPP noise prediction computer code for advanced subsonic propulsion systems, (1996)
  • [7] HOUGH J W, WEIR D S., Aircraft noise prediction program (ANOPP) fan noise prediction for small engines, (1996)
  • [8] ENVIA E,, NALLASAMY M., Design selection and analysis of a swept and leaned stator concept, Journal of Sound and Vibration, 228, 4, pp. 793-836, (1999)
  • [9] ZHANG Weiguang, WANG Xiaoyu, DU Lin, Et al., Mutual effect between swept-and-leaned vanes and acoustic liners on fan interaction-noise reduction, AIAA Journal, 57, 6, pp. 2479-2488, (2019)
  • [10] ZHANG Weiguang, Three-dimensional sound source model for fan noise with predictions and control methods, (2016)